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Study of surface pitots for measuring turbulent skin friction at supersonic Mach numbers - Adiabatic wallCalibration of surface pitot tubes for measuring turbulent skin friction at supersonic speeds - adiabatic wall
Document ID
19660019925
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Hopkins, E. J. (NASA Ames Research Center Moffett Field, CA, United States)
Keener, E. R. (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 2, 2013
Publication Date
July 1, 1966
Subject Category
Aerodynamics
Report/Patent Number
NASA-TN-D-3478
Report Number: NASA-TN-D-3478
Accession Number
66N29215
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
SKIN FRICTION
CALIBRATION
TURBULENT BOUNDARY LAYER
ADIABAT
PITOT TUBE

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